Learjet 35 - Page 44

2B-20 Developed for Training Purposes Leerjet 35/36
February 2002
CAE SimuFlite
Trim Speed Check:
The trim speed monitor compares pitch trim rate with flap
position. During ground test, a flaps down signal is applied
to the trim speed controller and a flaps up signal applied to
trim speed monitor to simulate the high trim rate with trim
speed monitor in low rate.
On aircraft with AAK 83-2:
Either Control Wheel Trim. . . . . . . . NOSE UP OR NOSE DN
TRIM OVSP-OFF-TRIM MON Switch. . . . . . . . . TRIM OVSP
Ensure amber PITCH TRIM annunciator illuminates.
TRIM OVSP-OFF-TRIM MON Switch. . . . . . . . . . .RELEASE
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DN
Either Control Wheel Trim. . . . . . . . NOSE UP OR NOSE DN
Ensure PITCH TRIM indicator needle moves faster with
flaps down. The trim-in-motion audio clicker does not sound.
On S/Ns 35-408, 506 and subsequent; 36-054 and
subsequent:
TEST Selector Switch. . . . . . . . . . . . . . . . . . . . . TRIM OVSP
Either Control Wheel Trim. . . . . . . . NOSE UP OR NOSE DN
TEST Button . . . . . . . . . . . . . .DEPRESS WHILE TRIMMING
Ensure amber PITCH TRIM annunciator illuminates.
TEST Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
Either Control Wheel Trim. . . . . . . . NOSE UP OR NOSE DN
Ensure PITCH TRIM indicator needle moves faster with
flaps down and the trim-in-motion audio clicker does not
sound.